更多"[单选题]In case of altitude failure, w"的相关试题:
[单选题]What will happen in case of a terrain warning？
A. The GPWS warning appears with “TERRAIN ALERT” aural warning.
B. “TERRAIN ALERT，PULL UP” aural warning continuously appears with corresponding red GPWS warning, and red “TERR AHEAD” message is displayed on ND.
C. The amber G/S warning appears and dark red “TERR” message is displayed on ND.
[单选题]On what cabin altitude will digital presentation pulses?
A. Above or equal to 9550 feet.
B. Above or equal to 8600 feet.
C. Above or equal to 8800 feet.
[单选题]What is the altitude range of ALPHA FLOOR?
A. This protection is available from lift-off to 100 ft RA on approach
B. This protection is available from lift-off to landing
C. This protection is available from 100 ft from lift-off to 100 ft RA on approach
[单选题]In case of aircraft failure affecting landing distance occurs in the air, the required landing distance can be calculated by reference to
A. the FCOM or the MEL
B. the FCOM and the QRH
C. the MEL only
[单选题]In case of ADR 1 failure,
A. set AIR DATA switch to CAPT3 position
B. set ATT HDG switch to CAPT 2 position
C. set AIR DATA and ATT HDG switches to NORM position
[单选题]In case of DMC failure, set the EIS DMC switching selector on the switching panel to APT 3 position, so as to replace _____ with DMC 3.
A. DMC1
B. DMC2
C. DMC1 and DMC2
[单选题]What will happen during EMER GEN test？
A. If Hot Bus2 Supplied and the green electric pump is running. The EMER GEN will be driven.
B. The RAT extends.
C. The EMER GEN is driven hydraulically if the blue electric pump is running.
[单选题]What will happen when active lane and auxiliary lane of air conditioning pack controller failure?
A. Using anti-icing valve to control outlet temperature of air-conditioning unit at 15 ℃.
B. Air conditioning unit is closed
C. Keep at failure temperature
[单选题]What is the indication of DMC failure？
A. “INVALID DATA” information is displayed on relevant DU
B. Relevant DU goes black
C. An amber cross is displayed on relevant DU
[单选题]What will happen if the thrust levers are not at idle during engine start?
A. The engine will not start.
B. The engine will start and rapidly accelerate to generate the thrust demanded by the TL
C. The engine will start and the thrust will be maintained at idle automatically.
[单选题]what will happen when in Configuration 1 + F and the airspeed is at 210 kt
A. the flaps retract to 0 ° automatically ,the new configuration is 1
B. flap automatically extend because of high airspeed
C. AOA protection is engaged because of high airspeed
[单选题]When it detects smoke ，what will happen， besides a single chime sounds； MASTER CAUTION lights light up and the ECAM displays a caution on the E/WD
A. The SMOKE light, on the EMER ELEC PWR panel, lights up
B. The BLOWER and EXTRACT FAULT, on the VENTILATION panel, light up.
C. The SMOKE light, on the EMER ELEC PWR panel, lights up；The BLOWER and EXTRACT FAULT, on the VENTILATION panel, light up.
[单选题]What will happen at approximately 43% N2 during manual starting?
A. The ON light on the MAN START PB button goes off.
B. The EEC sends a signal to the ECAM to close the start valve.
C. The start valve closes automatically.
[单选题]What will happen if Hot-Air Pressure-Regulating Valve failure and is in ON position？
A. Optimize regulation failure
B. Temperature is kept at the selected value when failure occurred.
C. No effect
[单选题]If FLAP1 is inoperative,what will happen？
A. nothing
B. flaps operate at half speed.
C. FLAP FAIL
[单选题]If one SFCC is inoperative, what will happen？
A. nothing
B. slats and flaps both operate at half speed.
C. FLAP FAIL
[单选题]What will happen if the C.G. is not at the proper position?
A. It may cause the aircraft body to tilt up or down or difficulty in directional control during taxi and takeoff roll due to loss of weight on nose gear wheels.
B. It will cause a large deviation of the pitch trim from the normal position, which will lead to an aerodynamically unstabilized situation of the aircraft.
C. Both of the above.
[单选题]Maximum altitude is：
A. The altitude at which the airplane covers the maximum distance per kilogram (pound) of fuel (best specific range).
B. The highest altitude the aircraft can reach with step clim
C. The maximum altitude at maximum cruise thrust in level flight and maximum altitude at maximum climb thrust with 300 ft/min vertical speed and 0.3 g margin.
